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陶瓷/复合材料航空装甲撞击响应的数值仿真
引用本文:龚尧南,钱纯,张佐光.陶瓷/复合材料航空装甲撞击响应的数值仿真[J].航空学报,1995,16(1):93-98.
作者姓名:龚尧南  钱纯  张佐光
作者单位:北京航空航天大学固体力学所, 北京, 100083
摘    要:用求解接触撞击问题的方法对陶瓷/复合材料装甲的撞击响应和失效机理进行数值仿真。着重讨论了接触撞击界面的搜索与确定、接触撞击力的计算、以及失效准则及其处理技巧等3个问题。计算结果与试验结果进行了比较,符合良好。

关 键 词:接触载荷  数据仿真  复合材料  
收稿时间:1993-11-04
修稿时间:1994-09-28

NUMERICAL SIMULATION OF IMPACT RESPONSE OF ADVANCED COMPOSED CERAMIC/COMPOSITE AERO ARMOUR
Gong Yaonan,Qian Chun,Zhang Zuoguang.NUMERICAL SIMULATION OF IMPACT RESPONSE OF ADVANCED COMPOSED CERAMIC/COMPOSITE AERO ARMOUR[J].Acta Aeronautica et Astronautica Sinica,1995,16(1):93-98.
Authors:Gong Yaonan  Qian Chun  Zhang Zuoguang
Institution:Research Institute of Solid Mechanics, Beijing University of Aeronautics and Astronautics, Beijing, 100083
Abstract:The impact response and failure mechanism of the composed ceramic/composite armour are simulated numerically by use of the solution method to contact-impact problems. Emphasis is put on the searching and determination of the contact-impact interface between the projectile and armour, the algorithm for the contact-impact force calculation, the establishment of failure criterion and its implementation strategy. The computational results are compared and agreed well with those data resulted from test.
Keywords:contactload  data simulation  composites  
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